JP6799591B2 - Manufacturing method of welded members and use of members - Google Patents
Manufacturing method of welded members and use of members Download PDFInfo
- Publication number
- JP6799591B2 JP6799591B2 JP2018517512A JP2018517512A JP6799591B2 JP 6799591 B2 JP6799591 B2 JP 6799591B2 JP 2018517512 A JP2018517512 A JP 2018517512A JP 2018517512 A JP2018517512 A JP 2018517512A JP 6799591 B2 JP6799591 B2 JP 6799591B2
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- Prior art keywords
- welded
- joint
- metal
- piece
- welding
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 238000004519 manufacturing process Methods 0.000 title claims description 6
- 229910052751 metal Inorganic materials 0.000 claims description 70
- 239000002184 metal Substances 0.000 claims description 70
- 238000000034 method Methods 0.000 claims description 37
- 239000000463 material Substances 0.000 claims description 34
- 238000003466 welding Methods 0.000 claims description 26
- 239000011810 insulating material Substances 0.000 claims description 12
- 229910000831 Steel Inorganic materials 0.000 claims description 8
- 239000010959 steel Substances 0.000 claims description 8
- 238000000465 moulding Methods 0.000 claims description 6
- 229910052782 aluminium Inorganic materials 0.000 claims description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 5
- 238000004080 punching Methods 0.000 claims description 5
- 229910001369 Brass Inorganic materials 0.000 claims description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 4
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 4
- 239000010951 brass Substances 0.000 claims description 4
- 229910052802 copper Inorganic materials 0.000 claims description 4
- 239000010949 copper Substances 0.000 claims description 4
- 238000005520 cutting process Methods 0.000 claims description 4
- 229910052749 magnesium Inorganic materials 0.000 claims description 4
- 239000011777 magnesium Substances 0.000 claims description 4
- 229910001220 stainless steel Inorganic materials 0.000 claims description 4
- 239000010935 stainless steel Substances 0.000 claims description 4
- 229910010293 ceramic material Inorganic materials 0.000 claims description 3
- 239000002131 composite material Substances 0.000 claims description 3
- 230000000694 effects Effects 0.000 claims description 3
- 239000000853 adhesive Substances 0.000 claims description 2
- 230000001070 adhesive effect Effects 0.000 claims description 2
- 239000002390 adhesive tape Substances 0.000 claims description 2
- 239000004568 cement Substances 0.000 claims description 2
- 238000010894 electron beam technology Methods 0.000 claims description 2
- 239000000835 fiber Substances 0.000 claims description 2
- 239000012530 fluid Substances 0.000 claims description 2
- 238000010097 foam moulding Methods 0.000 claims description 2
- 238000001746 injection moulding Methods 0.000 claims description 2
- 229920000642 polymer Polymers 0.000 claims description 2
- 239000011248 coating agent Substances 0.000 claims 1
- 238000000576 coating method Methods 0.000 claims 1
- 238000010168 coupling process Methods 0.000 claims 1
- 230000002401 inhibitory effect Effects 0.000 claims 1
- 239000010410 layer Substances 0.000 description 36
- 238000005304 joining Methods 0.000 description 9
- 238000005260 corrosion Methods 0.000 description 4
- 230000007797 corrosion Effects 0.000 description 4
- 238000010030 laminating Methods 0.000 description 3
- 230000000149 penetrating effect Effects 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- VEXZGXHMUGYJMC-UHFFFAOYSA-M Chloride anion Chemical compound [Cl-] VEXZGXHMUGYJMC-UHFFFAOYSA-M 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 239000011229 interlayer Substances 0.000 description 1
- 238000003475 lamination Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 239000011150 reinforced concrete Substances 0.000 description 1
- 239000011265 semifinished product Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
Classifications
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- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/05—Interconnection of layers the layers not being connected over the whole surface, e.g. discontinuous connection or patterned connection
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P17/00—Metal-working operations, not covered by a single other subclass or another group in this subclass
- B23P17/04—Metal-working operations, not covered by a single other subclass or another group in this subclass characterised by the nature of the material involved or the kind of product independently of its shape
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- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
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- B32B15/00—Layered products comprising a layer of metal
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- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
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- B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
- B32B3/266—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by an apertured layer, the apertures going through the whole thickness of the layer, e.g. expanded metal, perforated layer, slit layer regular cells B32B3/12
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- B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
- B32B3/30—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by a layer formed with recesses or projections, e.g. hollows, grooves, protuberances, ribs
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- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/06—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the heating method
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- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
- B32B37/142—Laminating of sheets, panels or inserts, e.g. stiffeners, by wrapping in at least one outer layer, or inserting into a preformed pocket
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- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
- E04C2/02—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials
- E04C2/26—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials composed of materials covered by two or more of groups E04C2/04, E04C2/08, E04C2/10 or of materials covered by one of these groups with a material not specified in one of the groups
- E04C2/284—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials composed of materials covered by two or more of groups E04C2/04, E04C2/08, E04C2/10 or of materials covered by one of these groups with a material not specified in one of the groups at least one of the materials being insulating
- E04C2/292—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials composed of materials covered by two or more of groups E04C2/04, E04C2/08, E04C2/10 or of materials covered by one of these groups with a material not specified in one of the groups at least one of the materials being insulating composed of insulating material and sheet metal
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
- E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
- E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
- E04C2/36—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P2700/00—Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
- B23P2700/01—Aircraft parts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P2700/00—Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
- B23P2700/50—Other automobile vehicle parts, i.e. manufactured in assembly lines
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
- E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
- E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
- E04C2/3405—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by profiled spacer sheets
- E04C2002/3472—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by profiled spacer sheets with multiple layers of profiled spacer sheets
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
- E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
- E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
- E04C2002/3483—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by spacers stamped from the sheets
Landscapes
- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Ceramic Engineering (AREA)
- Textile Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Laser Beam Processing (AREA)
- Arc Welding In General (AREA)
- Resistance Welding (AREA)
- Welding Or Cutting Using Electron Beams (AREA)
- Connection Of Plates (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Manufacturing Of Electrical Connectors (AREA)
Description
本発明は、金属片を溶接して部材を製造する方法に関するものであり、金属片間に少なくとも1つの材料片を配置して溶接する。また、本発明は、本部材の使用に関するものである。 The present invention relates to a method of manufacturing a member by welding metal pieces, and at least one material piece is arranged between the metal pieces and welded. The present invention also relates to the use of the present member.
互いに固定された少なくとも2つの異なる材料を含む材料構成物は、自動車、商用車、バスまたは鉄道車両などの輸送機関製造分野においてますます重要になってきている。いわゆる「複合材料構造」において、常に適切な材料を適切な場所に適用する必要がある。しかしながら、従来の接合方法では、鋼をアルミニウムに接合する、あるいは鋼を炭素繊維に接合するといった異種材料の接合組合せにおいて限界に達している。他にも、使用する材料の腐食電位が異なるという問題がある。薄板または要素の間に直接的な接触がある場合、卑材料に腐食が起きるおそれがある。塩化物のように湿潤部分または溶解液がある場合、問題はさらに深刻になる。 Material constructs containing at least two different materials fixed to each other are becoming increasingly important in the field of transportation manufacturing such as automobiles, commercial vehicles, buses or rail vehicles. In the so-called "composite structure", it is always necessary to apply the right material to the right place. However, in the conventional joining method, the limit is reached in the joining combination of different materials such as joining steel to aluminum or joining steel to carbon fiber. Another problem is that the corrosion potentials of the materials used are different. If there is direct contact between the sheet steel or the elements, the base material may corrode. The problem is exacerbated when there is a wet area or solution, such as chloride.
英国特許第1363536号は、パネル平面から貫入するたくさんのタブを全タブがパネルシートの平面に立った状態で使用する結合体に適用されパネルの厚さの総計よりも厚さ寸法が大きい構造用パネルについて記載している。さらに、タブは相互に取付け可能なため、2枚の薄板間に延びる1対の中間タブ間の結合が強固である。英国特許第1363536号は、パネルの強度を高めるためにパネルシートに対するタブの垂直位置および穿孔に関連して形成される一対のタブを示している。当該構造では、パネル層を2枚だけ相互に結合させている。 UK Pat. No. 1363536 applies to joints that use many tabs penetrating from the panel plane with all tabs standing on the plane of the panel sheet, for structures that are thicker than the total thickness of the panel. Describes the panel. Further, since the tabs are interchangeable, the bond between the pair of intermediate tabs extending between the two thin plates is strong. British Patent No. 1363536 indicates a pair of tabs formed in connection with the vertical position of the tabs with respect to the panel sheet and perforations to increase the strength of the panel. In this structure, only two panel layers are bonded to each other.
本発明の目的は、従来技術における問題点を解消し、互いに溶接される金属片間に少なくとも1つの材料片が配置された溶接部材の製造方法を達成することである。また、本発明は、上記部材の使用を目的とする。本発明の基本的な特徴は、添付の本願特許請求の範囲に記載する。 An object of the present invention is to solve a problem in the prior art and to achieve a method for manufacturing a welded member in which at least one material piece is arranged between metal pieces to be welded to each other. Moreover, this invention aims at use of the said member. The basic features of the present invention are described in the appended claims.
本発明によると、互いに溶接される金属片の少なくとも一方に、少なくとも1つの突起部が設けられる。溶接される金属片間に配置される少なくとも1つの材料片に、少なくとも1つの開口部が設けられ、互いに溶接される金属片の一方の金属片の突起部の少なくとも一部分が、開口部を貫通する。これにより、突起部の上端を介して、溶接される他方の金属片と機械的に接触する。金属片の溶接は、溶接される第1の金属片の突起部に接続する第2の金属片の表面に対して溶接効果をもたらすことによって行う。 According to the present invention, at least one protrusion is provided on at least one of the metal pieces to be welded to each other. At least one piece of material placed between the pieces of metal to be welded is provided with at least one opening, and at least a portion of the protrusions of one piece of metal to be welded to each other penetrates the opening. .. This causes mechanical contact with the other piece of metal to be welded through the top edge of the protrusion. Welding of a metal piece is performed by providing a welding effect on the surface of the second metal piece connected to the protrusion of the first metal piece to be welded.
このように、本発明によって製造された部材において、互いに溶接される金属片の少なくとも一方に少なくとも1つの突起部が設けられ、突起部の上端によって、溶接される第2の金属片と機械的に接触する。本発明の説明において、用語「第1の金属片」とは突起部を有する金属片を指し、用語「第2の金属片」とは突起部の上端が機械的に接触するもう一方の金属片を指す。本発明の説明において、用語「突起部の上端」とは、溶接を行う前に一方の金属片に固定される突起部の端部とは反対側の突起部の端部を指す。本発明の一実施例において、両金属片に突起部が設けられ、一方の金属片の突起部は他方の金属片の突起部と向かい合っていない。 As described above, in the member manufactured by the present invention, at least one protrusion is provided on at least one of the metal pieces to be welded to each other, and the upper end of the protrusion mechanically matches the second metal piece to be welded. Contact. In the description of the present invention, the term "first metal piece" refers to a metal piece having a protrusion, and the term "second metal piece" is another metal piece with which the upper end of the protrusion mechanically contacts. Point to. In the description of the present invention, the term "upper end of the protrusion" refers to the end of the protrusion opposite to the end of the protrusion fixed to one metal piece before welding. In one embodiment of the present invention, both metal pieces are provided with protrusions, and the protrusions of one metal piece do not face the protrusions of the other metal piece.
少なくとも1つの開口部が設けられた材料片は、中間層として、溶接される金属片の間に配置されるものである。材料片の開口部は、互いに溶接される金属片の一方の突起部の少なくとも一部が貫通できる形状である。突起部は開口部に対して配置されるため、突起部と開口部との直接的な接触をすべて防止できる。よって、開口部を貫通する突起部の部分は、溶接される第2の金属片の表面に機械的に接続される。金属片が互いに上述のように配置される場合、本発明による溶接は、溶接される金属片の突起部に接触する金属片の表面に作用する溶接効果に重点を置いて行われる。これにより、溶接された金属片間に配された少なくとも1つの材料片で構成される積層溶接部材を達成できる。 The material piece provided with at least one opening is arranged as an intermediate layer between the metal pieces to be welded. The opening of the material piece is shaped so that at least a part of one protrusion of the metal pieces welded to each other can penetrate. Since the protrusion is arranged with respect to the opening, all direct contact between the protrusion and the opening can be prevented. Therefore, the portion of the protrusion penetrating the opening is mechanically connected to the surface of the second metal piece to be welded. When the metal pieces are arranged with each other as described above, the welding according to the present invention is performed with an emphasis on the welding effect acting on the surface of the metal pieces in contact with the protrusions of the metal pieces to be welded. This makes it possible to achieve a laminated welded member composed of at least one piece of material arranged between the welded metal pieces.
本発明によると、本発明の方法は2つの材料を互いに直接接触させることなく3部構成部材として接合できるため、直接互いに溶接できない少なくとも3つの部分からなる材料の組合せの接合が可能である。したがって、開口部を備えた材料片は、閉鎖法として、または適合接続法として他の薄板に接合され、溶接される金属片は相互に物質的に接続される。よって、中間層材料と溶接された金属片との間の腐食に対する異なる電気化学電位は、本発明の方法によって製造された部材に直接的に関連しない。 According to the present invention, since the method of the present invention can join two materials as a three-part component without directly contacting each other, it is possible to join a combination of materials consisting of at least three parts that cannot be directly welded to each other. Thus, the pieces of material with openings are joined to other sheet steels as a closure method or as a conforming connection method, and the metal pieces to be welded are materially connected to each other. Thus, the different electrochemical potentials for corrosion between the interlayer material and the welded metal pieces are not directly related to the members manufactured by the methods of the invention.
本発明により溶接される金属片は、被覆鋼、ステンレス鋼、アルミニウム、マグネシウム、銅または真鍮から作られる。金属片は同種の材料からなるか、あるいは金属片は互いに溶接可能な材料の組合せから形成される材料からなる。金属片を互いに溶接する場合、抵抗溶接法、TIGスポット溶接法、またはレーザビーム溶接もしくは電子ビーム溶接などのビーム溶接法などの熱接合法によって行う。互いに溶接される金属片の少なくとも一方に少なくとも1つの突起部が設けられ、この場合、金属片は少なくとも一部が立体的である。突起部の形状は、円錐形、ピン形、テーパ形または他の任意の表面形状であり、溶接される他方の金属片との機械的に接触するのに有用である。有利には、金属片には複数の突起部が設けられ、突起部は、射出成形、クリンチング、円錐絞り加工、発泡成形または液圧成形などの成形法によって製造される。 The metal pieces welded according to the present invention are made of coated steel, stainless steel, aluminum, magnesium, copper or brass. The metal pieces are made of the same type of material, or the metal pieces are made of a material formed from a combination of materials that are weldable to each other. When metal pieces are welded to each other, they are welded by a thermal joining method such as resistance welding, TIG spot welding, or beam welding such as laser beam welding or electron beam welding. At least one of the metal pieces to be welded to each other is provided with at least one protrusion, in which case the metal pieces are at least partially three-dimensional. The shape of the protrusions can be conical, pin-shaped, tapered or any other surface shape and is useful for mechanical contact with the other piece of metal to be welded. Advantageously, the metal piece is provided with a plurality of protrusions, which are manufactured by molding methods such as injection molding, clinching, conical drawing, foam molding or hydraulic molding.
溶接される金属片の間に中間層として配置される材料片は、被覆鋼、ステンレス鋼、アルミニウム、マグネシウム、銅もしくは真鍮など金属ベースの材料からなるか、または繊維複合体もしくはセメント板からなる。中間層には少なくとも1つの開口部が設けられ、開口部の位置は金属片の突起に対して決められるため、突起部の少なくとも一部分が開口部を貫通することができ、これにより、中間層材とのあらゆる機械的な接触が防止される。有利には、中間層は複数の開口部を有し、開口部は中間層を穿孔して形成できる。中間層の穿孔は、打抜き、押抜き、中抜き、切削、またはレーザビームあるいはプラズマジェットおよびプラズマビームなどの熱切断によって作製できる。 The piece of material placed as an intermediate layer between the pieces of metal to be welded consists of a metal-based material such as coated steel, stainless steel, aluminum, magnesium, copper or brass, or a fiber composite or cement plate. Since the intermediate layer is provided with at least one opening and the position of the opening is determined with respect to the protrusion of the metal piece, at least a part of the protrusion can penetrate the opening, thereby allowing the intermediate layer material. Any mechanical contact with is prevented. Advantageously, the intermediate layer has a plurality of openings, which can be formed by perforating the intermediate layer. The perforation of the intermediate layer can be made by punching, punching, hollowing, cutting, or thermal cutting such as laser beam or plasma jet and plasma beam.
本発明によると、突起部を備えた金属片は、中間層の開口部に積み重ねられる。中間層の開口部の領域は、突起部の少なくとも一部分が開口部を貫通する形状であり、これにより、積層時および積層後に、中間層、突起部および金属片の間に接触が生じない。積層を行う前に、中間層と突起部との接触を防止するために、絶縁材の層を中間層の表面に塗布する。絶縁材は重合体、流動性接着剤、接着テープ、フリース素材入りテープ、可塑性絶縁材またはセラミック材である。絶縁材は、溶接される金属片と中間層材との間の電気化学的絶縁、電解腐食および接触腐食が発生する危険性を回避する。積層時、開口部と突起部の位置関係から、中間層の形態は固定され、接合される。金属層を積層して溶接した後、中間層を所望の方法により金属片間に圧入して、溶接部材を得る。 According to the present invention, the metal pieces provided with the protrusions are stacked in the openings of the intermediate layer. The region of the opening of the intermediate layer is shaped so that at least a portion of the protrusion penetrates the opening so that no contact occurs between the intermediate layer, the protrusion and the metal pieces during and after lamination. Prior to laminating, a layer of insulating material is applied to the surface of the intermediate layer to prevent contact between the intermediate layer and the protrusions. The insulating material is a polymer, a fluid adhesive, an adhesive tape, a tape containing a fleece material, a plastic insulating material or a ceramic material. The insulating material avoids the risk of electrochemical insulation, electrolytic corrosion and contact corrosion between the metal pieces to be welded and the intermediate layer material. At the time of stacking, the form of the intermediate layer is fixed and joined due to the positional relationship between the opening and the protrusion. After laminating and welding the metal layers, the intermediate layer is press-fitted between the metal pieces by a desired method to obtain a welded member.
本発明の方法によって製造された部材は、乗用車の横材、縦材、前壁、ピラー、床組立部または溝型材を相互に接合する結合部または接合部として用いられ、例えばBピラーとロッカーレールの結合部として使用される。また、本部材は、鉄道車両の側壁、フロアパネル、屋根またはステッププレートを相互に接合する結合部または接合部として用いることも可能であり、例えばフロアプレートと側壁との結合部として使用される。さらに、本部材を農業用機械、バスまたはトラックの薄板、板金、管、異形材を接合したり、航空宇宙飛行手段または宇宙飛行手段のプレートおよび薄板を接合したりする結合部または接合部として用いることも可能であり、例えばフロアプレートと側壁との結合部として使用できる。また、本部材は、例えば建造物の外殻構造と外観要素の結合部として建造物に使用可能であり、また、例えば鉄筋コンクリートの代替材料として橋および建造物に使用することもできる。 The members manufactured by the method of the present invention are used as joints or joints for joining passenger car cross members, vertical members, front walls, pillars, floor assembly parts or grooved members to each other, for example, B pillars and rocker rails. It is used as a joint part of. The member can also be used as a joint or joint for joining railroad vehicle side walls, floor panels, roofs or step plates to each other, for example, as a joint between a floor plate and a side wall. Furthermore, this member is used as a joint or joint for joining thin plates, sheet metal, pipes, and deformed materials of agricultural machinery, buses or trucks, and for joining plates and thin plates of aerospace flight means or space flight means. It is also possible, for example, as a joint between a floor plate and a side wall. The member can also be used in buildings, for example, as a joint between the outer shell structure of a building and exterior elements, and can also be used in bridges and buildings, for example, as an alternative material to reinforced concrete.
本発明の方法によって製造された部材を使用することにより、サンドイッチ板や注文部品の少なくともいずれかなど、半仕上げの製品を作製することも可能である。また、本発明の方法によって製造された部材を、少なくとも1つの他の部材に結合される適合部材として活用することもできる。 By using the members manufactured by the method of the present invention, it is also possible to produce semi-finished products such as sandwich plates and at least one of custom parts. Further, the member manufactured by the method of the present invention can also be utilized as a compatible member to be bonded to at least one other member.
本発明について、図面を参照して詳細に述べる。
図1において、中間層薄板1には孔2が設けられ、中間層1は2枚の金属薄板3および4の間に配置されている。金属薄板3は、突起部5が金属薄板3の表面に成形されるように構成されている。 In FIG. 1, the intermediate layer thin plate 1 is provided with a hole 2, and the intermediate layer 1 is arranged between two metal thin plates 3 and 4. The metal thin plate 3 is configured such that the protrusion 5 is formed on the surface of the metal thin plate 3.
図2において、金属薄板3および4は、突起部5が部分的に中間層1の孔を貫通するように積層される。金属薄板3および4は、突起部5の上端7によって機械的接触6を得る。中間層1と金属薄板3および4とを絶縁する絶縁材は図示しない。 In FIG. 2, the thin metal plates 3 and 4 are laminated so that the protrusions 5 partially penetrate the holes of the intermediate layer 1. The thin metal plates 3 and 4 obtain mechanical contact 6 by the upper end 7 of the protrusion 5. The insulating material that insulates the intermediate layer 1 and the thin metal plates 3 and 4 is not shown.
図3において、金属薄板11および12は、突起部13が部分的に中間層15の孔14を貫通するように積層される。中間層15を2つの絶縁材16および17によって支持することにより、突起部13と中間層15との間のあらゆる機械的な接触が防止される。 In FIG. 3, the thin metal plates 11 and 12 are laminated so that the protrusion 13 partially penetrates the hole 14 of the intermediate layer 15. By supporting the intermediate layer 15 with two insulating materials 16 and 17, any mechanical contact between the protrusion 13 and the intermediate layer 15 is prevented.
図4において、金属薄板21および22は、突起部23が部分的に中間層25の孔24を貫通するように積層される。中間層25を1つの絶縁材26によって支持することにより、突起部23と中間層25との間のあらゆる機械的な接触が防止される。 In FIG. 4, the thin metal plates 21 and 22 are laminated so that the protrusions 23 partially penetrate the holes 24 of the intermediate layer 25. By supporting the intermediate layer 25 with one insulating material 26, any mechanical contact between the protrusion 23 and the intermediate layer 25 is prevented.
図5において、金属薄板31および32は、突起部33が部分的に中間層35の孔を貫通するように積層される。中間層35を1つの絶縁材36によって支持することにより、突起部33と中間層35との間のあらゆる機械的な接触が防止される。また図5は、金属薄板31および32を互いに溶接する別の方法を示し、抵抗スポット溶接によって生じる溶接ナゲット37、レーザビーム法によって生じる溶接継目38、およびTIGスポット溶接法によって生じる溶接継目39を示す。 In FIG. 5, the thin metal plates 31 and 32 are laminated so that the protrusions 33 partially penetrate the holes of the intermediate layer 35. By supporting the intermediate layer 35 with one insulating material 36, any mechanical contact between the protrusion 33 and the intermediate layer 35 is prevented. FIG. 5 also shows another method of welding the metal sheets 31 and 32 to each other, showing the weld nugget 37 produced by resistance spot welding, the weld seam 38 produced by the laser beam method, and the weld seam 39 produced by the TIG spot welding method. ..
図6において、金属薄板41および42は、突起部43が部分的に中間層45の孔44を貫通するように積層される。絶縁材はいずれも図示していない。本発明による部材から注文品を製造するために、金属薄板41は別の部材47と結合する接合部46を有し、中間層45は本発明の部材の中間層45とは分離している中間層材49との接合部48を有する。 In FIG. 6, the thin metal plates 41 and 42 are laminated so that the protrusion 43 partially penetrates the hole 44 of the intermediate layer 45. None of the insulating materials are shown. In order to manufacture a custom product from a member according to the present invention, the thin metal plate 41 has a joint 46 to be bonded to another member 47, and the intermediate layer 45 is an intermediate layer separated from the intermediate layer 45 of the member of the present invention. It has a joint 48 with a layer material 49.
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Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3339017B1 (en) * | 2016-12-22 | 2020-11-25 | Outokumpu Oyj | Method for manufacturing a weldable metal-polymer multilayer composite |
CN109366035B (en) * | 2018-12-18 | 2020-04-14 | 安徽江淮汽车集团股份有限公司 | Resistance spot welding connection structure for steel-aluminum dissimilar materials |
US11471972B2 (en) | 2019-12-20 | 2022-10-18 | GM Global Technology Operations LLC | Combined stackup apparatus for resistance spot welding |
CN112709735A (en) * | 2020-12-29 | 2021-04-27 | 中国航空工业集团公司西安飞机设计研究所 | Composite material-metal integrated fusion joint |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3846218A (en) * | 1971-08-09 | 1974-11-05 | W Wootten | Fiber or paper board structure |
CA989577A (en) * | 1971-08-09 | 1976-05-25 | William A. Wootten | Structural panel and method of forming the same |
JPH09314353A (en) * | 1996-05-23 | 1997-12-09 | Toyota Autom Loom Works Ltd | Resistance welding method and construction of body to be welded |
JP3192619B2 (en) * | 1997-10-07 | 2001-07-30 | 日本特殊陶業株式会社 | Wiring board and method of manufacturing the same |
JP2001053438A (en) * | 1999-08-16 | 2001-02-23 | Sony Corp | Method for manufacturing multi-layer printed wiring board |
US6802682B2 (en) * | 2002-11-18 | 2004-10-12 | General Motors Corporation | Spiraled self-piercing rivet |
JP2006187786A (en) * | 2005-01-06 | 2006-07-20 | Hitachi Cable Ltd | Method for connecting titanium thin sheet and connected member connected by using the same |
US8466386B2 (en) * | 2006-10-10 | 2013-06-18 | GM Global Technology Operations LLC | Method for repairing bonded metallic structures |
JP2009285678A (en) * | 2008-05-28 | 2009-12-10 | Kobe Steel Ltd | Dissimilar material joining method and dissimilar material joined body between steel and light alloy, light alloy for joining dissimilar material for steel, and dissimilar material joining rivet between steel and light alloy |
JP4722193B2 (en) * | 2009-04-02 | 2011-07-13 | セキ工業株式会社 | Plate lamination structure, plate reinforcement structure, plate connection structure, and plate lamination method |
JP5856959B2 (en) * | 2009-09-25 | 2016-02-10 | シロー インダストリーズ インコーポレイテッド | Multilayer assembly having retention features |
DE102012102286A1 (en) * | 2012-03-19 | 2013-09-19 | Thyssenkrupp Steel Europe Ag | A method of bonding a composite sheet to a metallic substrate |
US9012029B2 (en) * | 2012-05-17 | 2015-04-21 | GM Global Technology Operations LLC | Method of bonding panels of dissimilar material and bonded structure |
DE102012218686A1 (en) * | 2012-10-15 | 2014-04-17 | Zf Friedrichshafen Ag | Component for a chassis of a vehicle |
EP2860407B1 (en) * | 2013-10-08 | 2017-01-18 | MAGNA STEYR Fahrzeugtechnik AG & Co KG | Structured component |
EP2859987B1 (en) * | 2013-10-08 | 2017-02-08 | MAGNA STEYR Fahrzeugtechnik AG & Co KG | Component Assembly |
WO2015117059A1 (en) * | 2014-02-03 | 2015-08-06 | Alcoa Inc. | Resistance welding fastener, apparatus and methods |
KR20160033879A (en) * | 2014-09-18 | 2016-03-29 | 주식회사 성우하이텍 | Self piercing projection welding rivet, joint structure and joint method using the same |
JP6043379B2 (en) * | 2015-02-25 | 2016-12-14 | 富士重工業株式会社 | Welding auxiliary member and spot welding method using the welding auxiliary member |
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2015
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Also Published As
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JP2018537287A (en) | 2018-12-20 |
AU2016336186A1 (en) | 2018-04-19 |
MX2018004069A (en) | 2018-08-01 |
EA201890609A1 (en) | 2018-11-30 |
BR112018006885A2 (en) | 2018-10-16 |
WO2017060229A1 (en) | 2017-04-13 |
PT3153315T (en) | 2020-10-09 |
CN108349217B (en) | 2020-12-01 |
CA3000299A1 (en) | 2017-04-13 |
CN108349217A (en) | 2018-07-31 |
EP3153315A1 (en) | 2017-04-12 |
HUE051032T2 (en) | 2021-01-28 |
KR20180056769A (en) | 2018-05-29 |
PL3153315T3 (en) | 2021-03-22 |
ZA201802234B (en) | 2019-07-31 |
ES2822908T3 (en) | 2021-05-05 |
EA037228B1 (en) | 2021-02-24 |
US20180281345A1 (en) | 2018-10-04 |
EP3153315B1 (en) | 2020-07-22 |
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